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Continuous combustion in gas turbine engines requires that a flame is held in a consistent location. Movement of the flame from the design location can be damaging and difficult to predict. Behaviours that precede the occurrence of flashback, the upstream movement of the flame, are found.
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This page is a summary of: Statistics and Dynamics of Intermittent Boundary Layer Flashback in Swirl Flames, Journal of Propulsion and Power, November 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b37815.
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